Phönix-Aviatechnica LKhS-4

Airplanes

Length

5.55 m

Flat Wing Span

8.2 m

Height

2.77 m

Max Seating

Cruise Speed

200 km/h

Max Speed

260 km/h

Max Ceiling

4000 m

Number of Engines

Maximum Take-Off Weight

0.82 t (paragliders: kg)

Maximum Range

500 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Phönix-Aviatechnica LKhS-4	0.82	500

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Durand et Delaville RB.01 Beauregard		5.25	8.26		Compare
Helmy Aerogypt	Continental O-170	5.7912	7.9248	3	Compare
Hodek HK-101	Walter Minor	5.91	7.7		Compare
Hollsmidt 222		5.83	8.87	1	Compare
Scaled Composites Pond Racer		6.096	7.62		Compare
Piel CP.500	Lycoming O-320	6.1	8.8	5	Compare

All data (19 fields)

Name: Phönix-Aviatechnica LKhS-4
Manufacturer: Phönix-Aviatechnica
Description: The Phönix-Aviatechnica LKhS-4 (also transliterated Phoenix-Aviatechnica LKhS-4 or Feniks-Aviatechnica LKhS-4; in Cyrillic script Феникс-Авиатехника ЛХС-4) was a 1990s Russian design for a civil utility aircraft of unusual configuration.
Designer: Phönix-Aviatechnica
Length (m): 5.55
Height (m): 2.77
Cockpit Crew: 1
Max Seating: 3
Max Speed (km/h): 260
Cruise Speed (km/h): 200
Max Ceiling (m): 4000
Rate of Climb (m/s): 6.4
Capacity Description: 3 passengers
National Origin: International joint venture: Russia and Bulgaria
Powerplant Description: 2 × VAZ-3187 two-cylinder piston engine, 60 kW (80 hp) each
Status: Unbuilt design
Wikipedia Article (URL): en.wikipedia.org/wiki/Ph%C3%B6nix-Aviatechnica_LKhS-4
Flat Wing Span (m): 8.2
Number of Engines: 2